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Turbulence Factors of NACA Wind Tunnels as Determined by Sphere TestsReport presents the results of drag and pressure tests of spheres having diameters of 2, 4, 6, 8, 10, and 12 inches in eight NACA wind tunnels, in the air ahead of the carriage in the NACA tank, and beneath an autogiro in flight .
Document ID
19930091633
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Platt, Robert C
Date Acquired
September 6, 2013
Publication Date
January 1, 1937
Report/Patent Number
NACA-TR-558
Report Number: NACA-TR-558
Accession Number
93R20923
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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